# Service difficulty reports: N950AT

A list on [N950AT](https://openairdocs.org/aircraft/N950AT.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 215 reports

- [SDR DALA2026090204949](https://openairdocs.org/sdr/DALA2026090204949.md): Threshold · damaged · Sep 2, 2026 · N950AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFT CARGO THRESHOLD FWD INBD CORNER STICKING UP AND DAMAGED, COMPLIED WITH ERA 636705-14. (9622032) (AIRCRAFT GROUNDED).
- [SDR DALA2026080604547](https://openairdocs.org/sdr/DALA2026080604547.md): Skin · dented · Aug 2, 2026 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENT FOUND ON THE FUSELAGE BTWN BS 218 - 229, COMPLIED WITH ER/A 636117-14. (1734913) (AIRCRAFT GROUNDED).
- [SDR DALA2026072204285](https://openairdocs.org/sdr/DALA2026072204285.md): Battery Pack · inoperative · Jul 21, 2026 · N950AT · Boeing 717200 · Emergency Lighting
  > OVERHEAD EXIT EMERGENCY LIGHT SIGN AND EMERGENCY LIGHT IN FWD GALLEY INOPERATIVE, R & R EMERGENCY BATTERY B5-259 IAW AMM 33- 51. (9127379) (AIRCRAFT GROUNDED).
- [SDR DALA2026072004263](https://openairdocs.org/sdr/DALA2026072004263.md): Relay · faulted · Jul 18, 2026 · N950AT · Boeing 717200 · Integrated Flight System
  > DIVERTED TO CVG DUE TO MULTIPLE FLIGHT DECK EFFECTS AFTER TAKEOFF. REPLACED LT PCDU, EMERGENCY POWER SWITCH AND EMERGENCY DC POWER RELAY. PERFORMED VERIFICATION FLIGHT. ALL OPS GOOD. (9127356) AIRCRAFT GROUNDED.
- [SDR DALA2026041702450](https://openairdocs.org/sdr/DALA2026041702450.md): Engine · fire · Apr 14, 2026 · N950AT · Boeing 717200 · Engine (Turbine/Turboprop)
  > FIRE- DURING RIGHT ENGINE START, TGT ROSE RAPIDLY ALONG WITH AUDIBLE STALL. ENGINE SHUTDOWN AND FIRE BOTTLE DISCHARGED. PERFORMED BORESCOPE INSPECTION OF LPC AND HPC, NO LIMITING DAMAGE FOUND. REPLACED NO.1 FIRE BOTTLE AND RETURNED TO SERVICE.(8685546) (AIRCR
- [SDR DALA2025120108775](https://openairdocs.org/sdr/DALA2025120108775.md): None · none · Nov 25, 2025 · N950AT · Boeing 717200 · Wing Structure
  > SHIP 9509 ER/A 623425-14AD REV C REQUIRES STAGE 2 DTA APRPOVAL. C/W ER/A 623425-14AD. (1321407)
- [SDR DALA2025070805067](https://openairdocs.org/sdr/DALA2025070805067.md): Pan · cracked · Jul 2, 2025 · N950AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9509 INITIAL INSPECTION: CRACK ON FWD EDGE INNER AND OUTER PAN DOOR BTW BEAM 1 AT AFT CARGO DOOR COMPARMENT. CORRECTIVE ACTION: FWD EDGE INNER AND OUTER PAN DOOR BTW BEAM 1 AT AFT CARGO DOOR COMPARMENT WERE REPAIRED PER ERA 626981-14 REV. ORIGINAL, SECTIO
- [SDR DALA2025062504749](https://openairdocs.org/sdr/DALA2025062504749.md): Frame Angle · corroded · Jun 24, 2025 · N950AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME ANGLES BTW LONG 28L & 28R AT STA Y=927 AFT CARGO COMPARTMENT. CORROSION LEVEL 2. FRAME ANGLES BTW LONG 28L & 28R AT STA Y=927 AFT CARGO COMPARTMENT. WERE REPLACED PER DWG 9919605-15.
- [SDR DALA2025062504748](https://openairdocs.org/sdr/DALA2025062504748.md): Intercostal · corroded · Jun 24, 2025 · N950AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS BTW STA Y=1022 & Y =1037 AT LONG 30 & LONG 29R BILGE AREA AT AFT CARGO COMPARTMENT. DAMAGED AREA REPAIRED PER B717-200 SRM 51-41-05- 0G AND SRM 51-41-02.
- [SDR DALA2025062504746](https://openairdocs.org/sdr/DALA2025062504746.md): Guide Vane · worn · Jun 23, 2025 · N950AT · Boeing 717200 · Trailing Edge Flaps
  > WEAR ON GUIDE VANE BEHIND HINGUE FLAP 1 AT RH WING. CORRECTIVE ACTION: GUIDE VANE WAS REPAIRED PER B717-200 SRM 57-53-01.
- [SDR DALA2025062104660](https://openairdocs.org/sdr/DALA2025062104660.md): Skin · dented · Jun 20, 2025 · N950AT · Boeing 717200 · Trailing Edge Flaps
  > DENT OUT OF LIMITS, AT LOWER SURFACE ON LH AFT MOVABLE FLAP VANE AT STA XF74 APROX (2 INCHES FROM T.E. AND 12 INCH FROM L.E.): W=WIDTH, Y =DEPTH (NO MORE 0.060 INCH), RATIO W/Y= MUST BE 10 OR MORE, DENT #17: W=2.0 INCH, Y=0.090 INCH AND W/Y= 22.22 PER B717-200
- [SDR DALA2025062004658](https://openairdocs.org/sdr/DALA2025062004658.md): Skin · corroded · Jun 20, 2025 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 9509, CORROSION AT LOWER SKIN DOOR JAMB ON MIDDLE DOORSTOP (AFT CARGO COMPARTMENT). CORRECTIVE ACTION: (CORROSION LEVEL 2) DOOR JAMB ON MIDDLE DOOR TOP (AFT CARGO COMPARTMENT) WAS REPLACED PER B717-200 SRM 51-41-02-0G, B717-200 SRM 51-41-05-0G AND B71
- [SDR DALA2025062004657](https://openairdocs.org/sdr/DALA2025062004657.md): Frame · cracked · Jun 19, 2025 · N950AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9509, CRACK ON FRAME STA Y1037 AND L13L AT PAX CABIN. CORRECTIVE ACTION: CRACK ON FRAME STA Y1037 AND L13L AT PAX CABIN. WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 1. (LP 1034104)
- [SDR DALA2025062004656](https://openairdocs.org/sdr/DALA2025062004656.md): Frame · cracked · Jun 19, 2025 · N950AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9509, CRACK ON FRAME STA Y1037 AND L13R AT PAX CABIN. CORRECTIVE ACTION: CRACK ON FRAME STA Y1037 AND L13R AT PAX CABIN. WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 1. (LP 1033875)
- [SDR DALA2025061904606](https://openairdocs.org/sdr/DALA2025061904606.md): Pan · cracked · Jun 19, 2025 · N950AT · Boeing 717200 · Passenger/Crew Doors
  > AIRCRAFT 9509, CRACK ON PAN NEAR TO BEAM NBR 2 AFT EDGE AT PASSENGER ENTRANCE DOOR. CORRECTIVE ACTION: PASSENGER ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP 1032719)
- [SDR DALA2025061904605](https://openairdocs.org/sdr/DALA2025061904605.md): Door Frame · corroded · Jun 18, 2025 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 9509, CORROSION WAS FOUND ON DOUBLERS REPAIR STA 954 AND 994 BTW S-26R TO S-27R AT LOWER SKIN DOOR JAMB ON AFT CARGO COMPARTMENT. CORRECTIVE ACTION: DOUBLERS REPAIR STA 954 AND 994 BTW S-26R TO S-27R AT LOWER SKIN DOOR JAMB ON AFT CARGO COMPARTMENT. W
- [SDR DALA2025061904604](https://openairdocs.org/sdr/DALA2025061904604.md): Seat Track · corroded · Jun 17, 2025 · N950AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 9509, CORROSION ON LH INB SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX. CORRECTIVE ACTION: CORROSION LEVEL 2 // LH INB SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX. WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-01-0G. (LP 1029594)
- [SDR DALA2025061904603](https://openairdocs.org/sdr/DALA2025061904603.md): Seat Track · corroded · Jun 17, 2025 · N950AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 9509, CORROSION ON INBD RH SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX. CORRECTIVE ACTION: CORROSION LEVEL 2 // INBD RH SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-01-0G. (LP 1029591)
- [SDR DALA2025061504505](https://openairdocs.org/sdr/DALA2025061504505.md): Longeron · cracked · Jun 13, 2025 · N950AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 9509, CRACK ON LONGERON 3(EAS) LONGERON 4, 5, AND 6 RH SIDE STA Y=1022 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: LONGERON 3(EAS) LONGERON 4, 5, AND 6 RH SIDE STA Y=1022 AT PASSENGER CABIN (CPAX) WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE
- [SDR DALA2025060904376](https://openairdocs.org/sdr/DALA2025060904376.md): Pan · cracked · Jun 8, 2025 · N950AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9509, AFTER SEAL RETAINERS REMOVAL, CRACK ON INNER PAN BTW STOP FITTING #1 AND #2 AFT EDGE, AT FWD CARGO DOOR WAS FOUND. CORRECTIVE ACTION: INNER PAN BTW STOP FITTING #1 AND #2 AFT EDGE, AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPA
- [SDR DALA2025060804360](https://openairdocs.org/sdr/DALA2025060804360.md): Cusp Web · corroded · Jun 7, 2025 · N950AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9509, CORROSION ON RH CUSP WEB UPPER & LOWER FACE ON STA Y=373 AT CABIN PAX. CORROSION LEVEL 2, CUSP WEB ON STA Y=373 AT CABIN PAX WAS REAPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP1011516)
- [SDR DALA2025052704024](https://openairdocs.org/sdr/DALA2025052704024.md): Inspection · none · May 21, 2025 · N950AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9509 COMPLY WITH ERA 623616-14AD RH WING/ REAR SPAR/ LOWER CAP CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 623616-14AD (0978229)
- [SDR DALA2025052704022](https://openairdocs.org/sdr/DALA2025052704022.md): None · none · May 18, 2025 · N950AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9509 INSTALL LH INBOARD AND CENTER BUTE DOORS. CORRECTIVE ACTION: C/W ER/A 623425-14AD (0972844)
- [SDR DALA2025052704021](https://openairdocs.org/sdr/DALA2025052704021.md): Structure · worn · May 18, 2025 · N950AT · Boeing 717200 · Fuselage, Wing Attach Fittings
  > SHIP 9509 LT WING OUTBD-AIRFRAME-HINGE BOLT HOLE IS WORN. CORRECTIVE ACTION: ALL WORK C/W ON ERA 625207 -14 REV ORG. (0973047)
- [SDR DALA2024123112105](https://openairdocs.org/sdr/DALA2024123112105.md): Spar · cracked · Dec 30, 2024 · N950AT · Boeing 717200 · Wing Spar
  > CRACK AT LEFT WING REAR SPAR, PRI 623253-14 REV 0 ISSUED. REMOVE TANK PLATES 520FT, 520CB, AND TWO FUEL LINES FOR MAINTENANCE. REMOVED AND REINSTALLED L/H OVER WING BOOST PUMP PANEL TO F.O.M. PER B717 AMM 28-00. RE-INSTALLED TANK PLATE 520CB PER B717 AMM 28-00
- [SDR DALA2024122712030](https://openairdocs.org/sdr/DALA2024122712030.md): Spar Cap · cracked · Dec 23, 2024 · N950AT · Boeing 717200 · Wing Spar
  > CRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP RADIUS. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. FC 5720-01103 2ND FASTENER INBOARD OF FLAP HINGE FITTING EXTERIOR FROM TRAILING EDGE THROUGH FASTENER INTO RADIUS. M
- [SDR DALA2023081406584](https://openairdocs.org/sdr/DALA2023081406584.md): Unknown · unknown · Aug 13, 2023 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > PUNCTURE IN FUSELAGE RT SIDE AFT OF FORWARD CARGO DOOR. THIS WAS ORIGINALLY DOCUMENTED IN LP #4849328 AND TRANSFERRED TO THIS LOG PAGE. MAINTENANCE REMOVED THE DAMAGE, DRILLED DOUBLER REF B717 53-03-01-2R PROCEDURE 1 REPAIR 1 CLASS 2 FIG 202 SHT 3, FABRICATED
- [SDR DALA2023070405377](https://openairdocs.org/sdr/DALA2023070405377.md): Unknown · unknown · Jul 3, 2023 · N950AT · Boeing 717200 · Emergency Lighting
  > THE CEILING EMERGENCY EXIT LIGHT COVER FELL OFF AT ROW 22. MAINTENANCE RESECURED THE LIGHTING COVER. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #8310082)
- [SDR DALA2023022501422](https://openairdocs.org/sdr/DALA2023022501422.md): None · none · Feb 23, 2023 · N950AT · Boeing 717200 · Fuselage Internal Mounting Structure
  > LT SLANT PANEL HAS CORROSION ON IT AT NUT PLATE LOCATION SEEN FROM THE INSIDE. BOTTOM ROW APPROX. LBL27. SUMMARY SEE NRC 001-0196:5300-2005/001 00276: COMPLIED WITH ER/A PRI 606032-14 REV "0","1" INSTRUCTIONAL STEPS. ENSURED FINAL ER/A 606032-14 REV ORIG SECTI
- [SDR DALA2023021401131](https://openairdocs.org/sdr/DALA2023021401131.md): Unknown · unknown · Feb 9, 2023 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > C/W ERA 597013-14 REV A FUSELAGE SKIN REPAIR AT LAV WASTE VENT. SUMMARY NRC 001-0002:2040-0015/001 00026: COMPLIED WITH ERA 597013-14 REV A FUSELAGE SKIN REPAIR AT LAV WASTE VENT. (LP #2621093)
- [SDR DALA2022051003229](https://openairdocs.org/sdr/DALA2022051003229.md): Door Sill · damaged · May 6, 2022 · N950AT · Boeing 717200 · Fuselage Floor Panel
  > FORWARD EDGE OF AFT CARGO DOOR FRAME SILL WAS DAMAGED BY BAGGAGE CREW WITH BELT LOADER. MAINTENANCE REMOVED DAMAGED SCUFF PLATE AND REFORMED PER B717 SRM 51-20-09-0G. INSPECTED SCUFF PLATE, NO CRACKS NOTED. COMPLIED WITH B717 SRM 53-00-15-2R. REINSTALLED SCUFF
- [SDR DALA2022042903018](https://openairdocs.org/sdr/DALA2022042903018.md): None · none · Apr 28, 2022 · N950AT · Boeing 717200 · Hydraulic System, Main
  > SHIP 9509 - THE FLIGHT CREW DECLARED AN EMERGENCY DURING LANDING DUE TO THE RIGHT HYDRAULIC QUANTITY SHOWING A LOW INDICATION (BUT NOT EMPTY). CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE #3 BRAKE PRESSURE LINE HAD BEEN DAMAGED BY A BIRD STRIKE AND WAS LEAKIN
- [SDR DALA2022021500951](https://openairdocs.org/sdr/DALA2022021500951.md): None · none · Feb 12, 2022 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE CROWN LIGHTNING STRIKE DAMAGE AT PREVIOUS BLEND OUT. NO REPAIR TAG PRESENT. -M-. SUMMARY SEE NRC 001-0249:5300-2018/003 00365: REPAIRED LIGHTNING STRIKE DAMAGE ON CROWN PER ER/A 597099-14 PRI REV. 0 THROUGH REV 1. AND ER/A 597099-14AD REV. ORIGINAL. (
- [SDR DALA2022021500949](https://openairdocs.org/sdr/DALA2022021500949.md): None · none · Feb 12, 2022 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION AROUND EXTERIOR SIDE OF VACUUM BLOWER FOR LAV TANK EXHAUST VENT -M-. SUMMARY SEE NRC 001-0247:2550-2003/001 00405: REPAIRED AREA AROUND VENT PER ER/A 597013-14 PRI REV 0 THROUGH REV 3 AND ER/A 597013-14 REV ORIGINAL. (LP #2118994)
- [SDR DALA2022021500945](https://openairdocs.org/sdr/DALA2022021500945.md): None · none · Feb 4, 2022 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > WHILE PERFORMING INSPECTION OF APU ENCLOSURE FWD SKIN ASSY. STA 1064 FOUND -2 REPAIR DOUBLER TO BE MISSING UPPER RH FASTENER PER ERA 540237-14 REV. O FIG. 2. SUMMARY SEE NRC 007-0001:21-0553-8- 7617/001 00320: REPAIRED PER ERA 540237-14 AND UPDATED LOG 2167684
- [SDR DALA2019020500805](https://openairdocs.org/sdr/DALA2019020500805.md): Fitting · corroded · Feb 4, 2019 · N950AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR FITTINGS G-7 (CPAX). CORROSION LEVEL 2, FLOOR FITTING OF G-7 WAS REPLACED PER ER/A 535099-14MA REV H AND CMM 25-30-16 REPAIR SECTION.
- [SDR DALA2019020400713](https://openairdocs.org/sdr/DALA2019020400713.md): Cargo Track · corroded · Feb 3, 2019 · N950AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > SEVERAL POINTS OF CORROSION ON LH TIE TRACK BTW STA 813 TO 1022 AT AFT CARGO COMPARTMENT (CCT). NRC 00271: CORROSION LEVEL 2, CORROSION ON TIE TRACK BTW STA 813 TO 1022 AT AFT CARGO COMPARTMENT WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26. (UT) WAS ACCOMPLI
- [SDR DALA2019020400711](https://openairdocs.org/sdr/DALA2019020400711.md): Cargo Track · corroded · Feb 3, 2019 · N950AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > SEVERAL POINTS OF CORROSION ON RH TIE TRACK BTW STA 813 TO 954 AT AFT CARGO COMPARTMENT (CCT). NRC 00272: CORROSION LEVEL 2, ON RH TIE TRACK BTW STA 813 TO 954 AT AFT CARGO COMPARTMENT (CCT), TIE TRACK WAS REPLACED PER B717-200 SRM 51-40-08-0G AND B717-200 SRM
- [SDR DALA2019020430710](https://openairdocs.org/sdr/DALA2019020430710.md): Doubler · corroded · Feb 2, 2019 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DURING INSPECTION OF A REPAIRED AREA AT FUSELAGE SKIN STA 851; L29L-29R, SOME CORROSION WAS FOUND. NRC 00225: REPAIR DOUBLER WAS REPLACED PER ER/A 540245-14 REV. ORIGINAL. ASSOCIATED ER/A 14-540245 ADDED FOR AC 9509. (LP #0929471)
- [SDR DALA2019020200708](https://openairdocs.org/sdr/DALA2019020200708.md): Access Panel · corroded · Feb 2, 2019 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON LAVATORY SERVICE ACCESS INNER PANE AT FUSELAGE. (FUS). NRC 00059: LAVATORY SERVICE ACCESS INNER PANE AT FUSELAGE WAS REPLACED PER B717-200 SRM 51-41-02 AND 51-41-05. (LP #0928367)
- [SDR DALA2019020430706](https://openairdocs.org/sdr/DALA2019020430706.md): Skin · corroded · Feb 2, 2019 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND AT FUSELAGE SKIN STA 851; L29L-29R. NRC 00225: REPAIR DOUBLER WAS REPLACED PER ER/A 540245-14 REV. ORIGINAL. PERFORM ACOMPLISH ER/A 540245-14 REV. ORIGINAL SECTION I. ASSOCIATED ER/A 14-540245 ADDED FOR AC 9509. (LP #0929473)
- [SDR DALA2019013100635](https://openairdocs.org/sdr/DALA2019013100635.md): Floor Support · corroded · Jan 30, 2019 · N950AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > EXFOLIATION TYPE CORROSION ON FLOOR SUPPORT STA 655 BTW L28L TO L28R 5331-2007 (CCD). NRC 00291: CORROSION LEVEL 2, SUPPORT WAS REPLACED PER SRM 51-41-02-0G AND DWG #5971111 REV. F. (LP #0925601)
- [SDR DALA2019013000624](https://openairdocs.org/sdr/DALA2019013000624.md): Doubler · corroded · Jan 29, 2019 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON PRODUCTION DOUBLER OF INNER SKIN FUSELAGE BTW STA Y=974 TO 954 AND L30 TO L29R AT AFT CARGO COMPARTMENT 5331-2001. NRC 00224: CORROSION LEVEL 2, PRODUCTION DOUBLER OF INNER SKIN FUSELAGE BTW STA Y=974 TO 954 AND L30 TO L29R WAS REPAIRED PER ETI-17
- [SDR DALA2019012901848](https://openairdocs.org/sdr/DALA2019012901848.md): Window Frame · cracked · Jan 28, 2019 · N950AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON LT SLIDE WINDOW FRAME UPPER AFT CORNER STA 120. NRC 00500: LT SLIDE WINDOW STIFFENER (BRACKET) UPPER AFT CORNER STA 120 WAS REPLACED PER SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. DOUBLER WAS INSTALLED PER SRM 51-41-05-0G AND 56-10-02-2R. (ET) HFE
- [SDR DALA2019030601500](https://openairdocs.org/sdr/DALA2019030601500.md): Skin · cracked · Jan 28, 2019 · N950AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > TWO CRACKS ON FWD TOP SKIN AND ONE CRACK ON UPPER RIGHT EDGE AT FWD WALL OF APU COMPARTMENT IN REF NRC 00369. (CAT). NRC 00513: CRACKS (2) ON FWD TOP SKIN AND CRACK (1) ON UPPER RIGHT EDGE AT FWD WALL OF APU COMPARTMENT IN REF NRC 00369 WERE REPAIRED PER ETI-1
- [SDR DALA2019012900620](https://openairdocs.org/sdr/DALA2019012900620.md): Longeron · not reported · Jan 28, 2019 · N950AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > REMOVE LONGERON 25L BETWEEN STA 974/994 (IN REF NRC 00059) FOR SPLICE REPAIR PER SRM 53-00-05-2R-2. LONGERON 25L WAS REPAIRED PER SRM 53-00-05-2R-2. (LP #0922514)
- [SDR DALA2019012800571](https://openairdocs.org/sdr/DALA2019012800571.md): Bracket · cracked · Jan 27, 2019 · N950AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON RT SLIDE WINDOW FRAME UPPER AFT CORNER STA 120. NRC 00499: RT SLIDE WINDOW STIFFENER (BRACKET) UPPER AFT CORNER STA 120 WAS REPLACED PER SRM 51-41-01-0G, 51-41-01-02-0G, AND 51-41-05-0G. (ET)(HFEC) WAS ACCOMPLISHED ON RT SLIDE WINDOW FRAME UPPER AFT C
- [SDR DALA2019012800570](https://openairdocs.org/sdr/DALA2019012800570.md): Floor Panel · corroded · Jan 27, 2019 · N950AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR PANEL STA 120 (CPAX). NRC 00514: CORROSION LEVEL 2, FLOOR PANEL STA 120 WAS REPLACED PER DWG #9957828 REV: Y. (UT) ACCOMPLISHED PER NDT 04-00-07 PAR. 5 FIG. 3 SHEET 1 AND 2 ON FLOOR PANEL STA 120. ORIGINAL THICKNESS IS 0.100" AND MAXIMUM REM
- [SDR DALA2019012800569](https://openairdocs.org/sdr/DALA2019012800569.md): Splice · corroded · Jan 27, 2019 · N950AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION TYPE EXFOLIATION ON SPLICE STA Y=898.500 BTW L27R TO L26L AT AFT CARGO COMPARTMENT AMDS 5331-2001. (CCT). NRC 00165: CORROSION LEVEL 2. SPLICE STA Y=898.500 BTW L27R TO L26L WAS REPLACED PER SRM 51-41-05. (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PA
- [SDR DALA2019012900621](https://openairdocs.org/sdr/DALA2019012900621.md): Beam · cracked · Jan 26, 2019 · N950AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON RT NLG DOOR JAMB BEAM STA Y=40. (NLG). NRC 00155: RT NLG DOOR JAMB BEAM STA Y=40 WAS REPAIRED PER ER/A 495600-14MA REV. C.(ET)(HFEC) WAS ACCOMPLISHED ON RT NLG DOOR JAMB BEAM STA Y=40.(NLG) AND CRACK WAS DIMENSIONED WITH 1.500" LENGTH PER NDTSPM 06-10

Next page: https://openairdocs.org/aircraft/N950AT/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N950AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N950AT/reports

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